The overall objective of the design effort was to conduct a preliminary vehicle-sizing activity to establish baseline configurations for the STOL tactical aircraft investigation. These preliminary baselines were used for the takeoff and landing studies and as a point of departure for wind tunnel test planning and flight control technology activities. The lift/propulsion concepts studied were: Externally Blown Flap (EBF); Mechanical Flap plus Vectored Thrust (MF/VT); and Internally Blown Flap (IBF). The report summarizes the design activities for the three-month and six-month configuration reviews.


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    Title :

    STOL Tactical Aircraft Investigation. Volume I. Configuration Definition


    Contributors:
    J. Hebert (author) / C. Whitney (author) / R. E. Johnston (author) / G. B. Nicoloff (author) / E. C. Laudeman (author)

    Publication date :

    1973


    Size :

    169 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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